Path: Orbit/RHSOrbit
% Two dimensional orbit dynamics.
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Form:
xDot = RHSOrbit2D( x, t, d )
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Inputs
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x (4,1) [r;v]
t (1,1) Time (unused)
d (1,1) Data structure
.mu (1,1) Gravitational potential
.a (2,1) External acceleration
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Outputs
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xDot (4,1) d[r;v]/dt
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Math: Linear/Mag
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